θ

Inclined & Horizontal Plate Natural Convection

Analyze natural convection boundary layers on flat plates oriented at arbitrary angles from vertical.

Gravity (g) Plate (Ts) Length L θ = 45°

Effective Gravity and Angle

For inclined plates ($\theta < 90^\circ$ from vertical), natural convection correlations are modified by replacing the standard gravity constant $g$ with the effective parallel component: $$g_{eff} = g \cos \theta$$ For horizontal plates ($\theta = 90^\circ$), fluid buoyancy forces form rising plumes (on upper hot/lower cold surfaces) or stable stratification layers (on lower hot/upper cold surfaces).

Parameters Setup

📐 Geometry & Orientation
🌡️ Temperatures
↔️ Boundary & Fluid

Results & Curves

4.197e+8
Rayleigh Ra
94.1309
Nusselt Nu
4.9513
h [W/m²K]
40.8481
Heat rate Q [W]

📈 Nusselt number vs Temperature difference (dT)

Engine Output

============================================
  INCLINED & HORIZONTAL PLATE CONVECTION
============================================

  Rayleigh Number Ra      =     4.1974E+08
  Nusselt Number Nu       =      94.1309
  Coeff h                 =       4.9513 W/m2K
  Transfer Q              =      40.8481 W

--- DELTA-T SWEEP ---
  dT[C]      Ra           Nu        h[W/m2K]   Q[W]
  ------------------------------------------------------------
      1.00   7.632E+06     28.913      1.5208        0.2281
      7.83   5.978E+07     52.419      2.7572        3.2397
     14.67   1.119E+08     63.154      3.3219        7.3082
     21.50   1.641E+08     70.825      3.7254       12.0143
     28.33   2.162E+08     76.966      4.0484       17.2058
     35.17   2.684E+08     82.165      4.3219       22.7978
     42.00   3.205E+08     86.713      4.5611       28.7349
     48.83   3.727E+08     90.781      4.7751       34.9774
     55.67   4.248E+08     94.477      4.9695       41.4955
     62.50   4.770E+08     97.877      5.1483       48.2655
     69.33   5.291E+08    101.032      5.3143       55.2684
     76.17   5.813E+08    103.982      5.4694       62.4883
     83.00   6.334E+08    106.757      5.6154       69.9117
     89.83   6.856E+08    109.380      5.7534       77.5270
     96.67   7.377E+08    111.871      5.8844       85.3244
    103.50   7.899E+08    114.246      6.0093       93.2948
    110.33   8.420E+08    116.516      6.1287      101.4304
    117.17   8.942E+08    118.692      6.2432      109.7243
    124.00   9.463E+08    120.784      6.3532      118.1701
    130.83   9.985E+08    122.799      6.4592      126.7621
    137.67   1.051E+09    124.743      6.5615      135.4950
    144.50   1.103E+09    126.624      6.6604      144.3642
    151.33   1.155E+09    128.444      6.7562      153.3650
    158.17   1.207E+09    130.210      6.8490      162.4936
    165.00   1.259E+09    131.925      6.9392      171.7462

Calculation Methodology

Mathematical Model & Theory

Natural convection on inclined flat plates is calculated using Churchill & Chu's vertical plate correlation with modified parallel gravity: $$g_{eff} = g \cos \theta$$ $$\text{Nu}_L = \left\{0.825 + \frac{0.387 \text{Ra}_L^{1/6}}{\left[1 + (0.492/\text{Pr})^{9/16}\right]^{8/27}}\right\}^2$$ For horizontal plates ($\theta = 90^\circ$), characteristic length is defined as: $$L_c = \frac{\text{Area}}{\text{Perimeter}} = \frac{L \cdot W}{2(L+W)}$$ Correlations for upper surface of hot plate / lower surface of cold plate: $$\text{Nu} = 0.54 \text{Ra}^{1/4} \quad (\text{Ra} < 10^7)$$ $$\text{Nu} = 0.15 \text{Ra}^{1/3} \quad (\text{Ra} \ge 10^7)$$ Correlations for lower surface of hot plate / upper surface of cold plate: $$\text{Nu} = 0.27 \text{Ra}^{1/4}$$

Academic References:

  1. Incropera, F. P., & DeWitt, D. P. (2011). Fundamentals of Heat and Mass Transfer. 7th Edition, John Wiley & Sons.
  2. Churchill, S. W., & Chu, H. S. (1975). Correlating Equations for Laminar and Turbulent Free Convection on a Vertical Plate. Int. J. Heat Mass Transfer.

Worked Engineering Example

Problem Statement:
A $0.5\text{ m} \times 0.3\text{ m}$ flat plate tilted at $30^\circ$ from vertical is maintained at $80^\circ\text{C}$ in ambient air at $25^\circ\text{C}$. Find the convection coefficient ($T_f = 52.5^\circ\text{C}$).

Step-by-step Solution:
1. Evaluate air properties at film temperature:
- $\nu = 1.83 \times 10^{-5}\text{ m}^2\text{/s}, \alpha = 2.6 \times 10^{-5}\text{ m}^2\text{/s}, k = 0.028\text{ W/m·K}, Pr = 0.71, \beta = 1/325.65 = 0.00307\text{ K}^{-1}$.
2. Calculate effective gravity:
$$g_{eff} = 9.81 \times \cos(30^\circ) = 8.495\text{ m/s}^2$$ 3. Compute Rayleigh number with $g_{eff}$ ($L_c = 0.5\text{ m}$):
$$\text{Ra}_L = \frac{g_{eff} \beta (T_s - T_a) L_c^3}{\nu \alpha} = \frac{8.495 \times 0.00307 \times (80-25) \times 0.5^3}{1.83 \times 10^{-5} \times 2.6 \times 10^{-5}} = 3.77 \times 10^8$$ 4. Compute Nusselt number using Churchill & Chu correlation:
$$\text{Nu}_L = \left\{0.825 + \frac{0.387 \times (3.77 \times 10^8)^{1/6}}{\left[1 + (0.492/0.71)^{9/16}\right]^{8/27}}\right\}^2 = \left\{0.825 + \frac{10.37}{1.157}\right\}^2 = 95.8$$ 5. Calculate convective coefficient $h$:
$$h = \frac{\text{Nu}_L k}{L_c} = \frac{95.8 \times 0.028}{0.5} = 5.36\text{ W/m}^2\text{K}$$